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SERVICE BULLETIN Service Bulletin No SERVICE BULLETIN Service Bulletin No. 075 2900 Selma Highway Montgomery, AL 36108 USA Alternator Drive Coupling Inspection Tel: 334-386-5400 Fax: 334-386-5450 1. Planning Information A. Effectivity (1) Plane-Power Jasco series alternators manufactured by Hartzell Engine Technologies (HET) and Skytronics Inc. PNs 6555(T, C), 6565(T, C), 7555(T, C), 7565(T, C), and 7655(T, C) are affected by this Service Bulletin (SB). (a) 6555(T, C) serial numbers H-S060104 and prior are affected by this SB. (b) 6565(T, C) serial numbers H-S060108 and prior are affected by this SB. (c) 7555(T, C) serial numbers H-S060118 and prior are affected by this SB. (d) 7565(T, C) serial numbers H-S051413 and prior are affected by this SB. (e) 7655(T, C) serial numbers H-S050284 and prior are affected by this SB. (2) Aircraft Type/Model and alternator part numbers affected by this SB are shown in Table 1 – Alternator/Aircraft Effectivity. NOTE: Table 1 is for reference only and is not an all-inclusive list of aircraft affected by this SB. It is the responsibility of the owner/operator to verify whether an affected alternator may be installed. WARNING: DO NOT USE OBSOLETE OR OUTDATED INFORMATION. PERFORM ALL INSPECTIONS OR WORK IN ACCORDANCE WITH THE MOST RECENT REVISION OF THIS SERVICE BULLETIN. INFORMATION CONTAINED HEREIN MAY BE SIGNIFICANTLY CHANGED FROM EARLIER REVISIONS. FAILURE TO COMPLY WITH THIS SERVICE BULLETIN OR THE USE OF OBSOLETE INFORMATION MAY CREATE AN UNSAFE CONDITION THAT MAY RESULT IN DEATH, SERIOUS BODILY INJURY, AND/OR SUBSTANTIAL PROPERTY DAMAGE. REFER TO THE PLANE-POWER WEBSITE, WWW.PLANEPOWER.AERO, FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN. B. Concurrent Requirements (1) None C. Reason (1) HET has discovered alternators containing part numbers listed in section 1.A. of this SB contain a condition that has potential, if not corrected, to introduce foreign object debris (FOD) into the engine cavity. Rev. New: 27 Sept. 2018 SB 075 © 2018 - Hartzell Engine Technologies - All rights reserved Page 1 of 9 SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection D. Description (1) This Service Bulletin provides Instructions for Continued Airworthiness (ICA). (2) This Service Bulletin provides instructions for inspection and replacement of affected alternator drive coupling components. E. Compliance (1) Compliance with section 3.A of this SB is required within twenty-five (25) hours time-in- service from the release date of this SB or at the next regularly scheduled inspection, whichever occurs first. (2) Compliance with section 3.B of this SB is required no later than two hundred and fifty (250) hours time-in-service from the release date of this SB. (3) Compliance with the Accomplishment Instructions is the terminating action for this Service Bulletin. F. Approval (1) FAA acceptance has been obtained on the technical data in this publication that affects type design. G. Manpower (1) Two (2.0) man hours of labor are needed for removal, inspection, and installation of the alternator. (2) One (1.0) man hour of labor is needed for removal, inspection, and replacement of affected alternator drive coupling components. H. References (1) Applicable aircraft POH or AFM (2) Aircraft maintenance manual (as applicable). I. Weight and Balance (1) No Change 2. Material Required A. New or overhauled Jasco alternator not affected by this SB. B. See Table 2 for field-replacement components. SB 075 Rev. New: Sept. 27, 2018 Page 2 of 9 © 2018 - Hartzell Engine Technologies - All rights reserved SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection Alternator PN Aircraft Make Aircraft Model/Series Cessna 150, 170, 172, 175 IAW STC SA971WE A188, A, B modified IAW Air Repair, Inc. STC Cessna 6555(T, C) SA2279SW 190, 195, A, B modified IAW Air Repair, Inc. STC Cessna SA1809SW H-295 (USAF U-10D), HT-295, H391 (USAF L-28A 6565(T, C) Cessna or U-10B) modified IAW JAARS STC SA987SO US Army OH-13H, Tomcat Mark 5A, Mark 6B Texas Helicopter modified IW Texas Helicopter Comin Inc. IAW STC Company, Inc. SH2303SW 7555(T, C) Thrush Aircraft S-2R, S2R-R1340 A188, A, B modified IAW Air Repair, Inc. IAW STC Cessna SA2279SW 7565(T, C) Emair MA-1B Weatherly Aviation 620A, 620B 7655(T, C) Company, Inc Air Tractor Inc. AT-300, AT-301, AT-401, AT-401B, AT-501 Alternators Purchased as Part of a Kit - Kits include alternator 6555(T, C) or 7555(T, C) Alterntor Kit PN Aircraft Make Aircraft Model Series PN Grumman G164A - with STC SA2015WE installed 6555-1 6555(T, C) 35, A35, B35, C35, D35, E35, F35, 35R IAW STC Beech SA999WE Bell 47G, 47G2 - with STC SH191WE installed 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, Bell 47G-3B-2, 47G03B-2A, 47G-4, 47G-4A, 47G-5, 7555-1 7555(T, C) 47G-5A - with STC SH193WE installed 47J, 47J2, 47J2A, 47K - with STC SH194WE Bell installed Grumman G164A - with STC SA2015WE installed Table 1 - Alternator/Aircraft Effectivity Rev. New: Sept. 27, 2018 SB 075 © 2018 - Hartzell Engine Technologies - All rights reserved Page 3 of 9 SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection 5 4 7 6 3 2 1 Alternator / Quantity Item No. Part Number Description 6555(T, C) 6555(T, 7555(T, C) 7555(T, C) 7565(T, 6565(T, C) 6565(T, C) 7655(T, 1 MS24665-132 Cotter Pin 1 1 1 2 AN320-5 Nut, (Castle)▲ 1 1 1 2 NAS1291C5M Nut, Self Locking 1 1 3 NAS1149F0563P Washer, Flat ▲ 1 1 1 1 1 4 669 Gear, Drive ▲ 1 1 1 4 689 Gear, Drive ▲ 1 1 5 626543SKY Bushing 2 2 2 2 2 6 668-2 Retainer ▲ 1 1 1 1 1 7 671 Hub ▲ 1 1 1 1 1 NOTE 1: Circled Item Numbers are required replacement parts per affected alternator. NOTE 2: ▲ On-condition items. Replace if worn or damaged. Table 2 - Materials Required SB 075 Rev. New: Sept. 27, 2018 Page 4 of 9 © 2018 - Hartzell Engine Technologies - All rights reserved SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection 3. Accomplishment Instructions WARNING 1: THIS PROCEDURE MUST BE PERFORMED BY COMPETENT AND QUALIFIED PERSONNEL WHO ARE FAMILIAR WITH THE AIRFRAME AND ENGINE SYSTEM MAINTENANCE. FAILURE TO DO SO MAY RESULT IN PHYSICAL INJURY, EQUIPMENT DAMAGE AND/OR ECONOMIC LOSS. WARNING 2: DO NOT USE OBSOLETE OR OUTDATED INFORMATION. PERFORM ALL INSPECTIONS OR WORK IN ACCORDANCE WITH THE MOST RECENT REVISION OF THIS SERVICE BULLETIN. INFORMATION CONTAINED HEREIN MAY BE SIGNIFICANTLY CHANGED FROM EARLIER REVISIONS. FAILURE TO COMPLY WITH THIS SERVICE BULLETIN OR THE USE OF OBSOLETE INFORMATION MAY CREATE AN UNSAFE CONDITION THAT MAY RESULT IN DEATH, SERIOUS BODILY INJURY, AND/OR SUBSTANTIAL PROPERTY DAMAGE. REFER TO THE plane-power WEBSITE FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN, WWW.PLANEPOWER.AERO. CAUTION: REFER TO THE APPLICABLE MANUFACTURER’S MAINTENANCE MANUALS OR SERVICE INSTRUCTIONS TO GAIN ACCESS TO THE AIRFRAME OR alternator. IN ADDITION, ANY PREFLIGHT OR IN-FLIGHT OPERATIONAL CHECKS REQUIRE USE OF THE APPROPRIATE AFM OR POH. A. Inspection (1) If previous compliance cannot be verified through aircraft or engine maintenance records, use the same references to determine if an affected alternator has been installed. Refer to section 1.A, Effectivity. (2) If effectivity of the alternator cannot be established using aircraft or engine maintenance records, utilize the applicable aircraft maintenance manual to gain access to the alternator and inspect the alternator serial number against affected serial numbers found in section 1.A of this SB. (3) If the alternator serial number is affected per section 1.A: (a) Utilize applicable aircraft maintenance manual to remove the alternator and inspect the alternator gear drive (Item Number 4, Table 2 – Materials Required) for correct alignment. Refer to Figures 1 & 2 - Alignment Inspection. 1) If INCORRECT alternator gear drive alignment is observed, continue to Corrective Action section 3.B.(1). 2) If CORRECT alignment is observed, the affected alternator may be re-installed on aircraft and re-inspected in accordance with section 3.A.(3) every fifty (50) hours time- in-service until a total of two hundred and fifty (250) hours time-in-service is reached from release date of this SB. Rev. New: Sept. 27, 2018 SB 075 © 2018 - Hartzell Engine Technologies - All rights reserved Page 5 of 9 SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection a) When a total of 250 hours time-in-service is reached from the release date of this SB, continue to Corrective Action section 3.B.(1) of this SB regardless of inspection findings. Figure 1 - CORRECT Alignment Figure 2 - INCORRECT Alignment Figures 1 & 2 - Alignment Inspection B. Corrective Action Refer to Item Numbers in Table 2 – Materials Required. (1) Disassembly (a) Disassembly of alternator PNs 6555(T, C), 7555(T, C), and 7655(T, C). 1) Remove Cotter Pin (1) from Gear Drive Nut (2) and discard. 2) Reference Figure 3 to fabricate a tool that will interface with nut castellations and remove Nut (2) from the gear shaft. Retain nut (2) and washer (3) for assembly. SB 075 Rev. New: Sept. 27, 2018 Page 6 of 9 © 2018 - Hartzell Engine Technologies - All rights reserved SERVICE BULLETIN Service Bulletin No. 075 Alternator Drive Coupling Inspection a) Hold base of Drive Gear (4) with a one inch crowfoot wrench or small strap wrench while removing Nut (2). 3) Remove Drive Gear (4) from gear shaft and retain for assembly. 4) Remove Bushings (5) from Retainer (6) and discard.
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